BRP ROTAX 916 i A Series User Manual

Effectivity: 916 i A / C24
Edition 0 / Rev. 1
BRP-Rotax Page 3-9
December 01 2023
Emergency En-
gine shut-off
Step Step Description Procedure
1 Deactivate ECU HIC A: Disconnect Terminal 1
and Terminal 7 at 916 i Type A,
or at 916 i Type C24 Terminal N
and P, to turn OFF ECU Lane A
HIC B: Disconnect Terminal 1
and Terminal 9 at 916 i Type A,
or at 916 i Type C24 Terminal n
and P, to turn OFF ECU Lane B
Display CAN A/B: Check and
ensure compliance with opera-
tional limits.
Example (Symbolic) Lane select Switch A: OFF
Lane select Switch B: OFF
Loss of Display
CAN Information
If Display CAN Bus A or B fail, all informations are still available
on the working CAN Bus. In case Display CAN A and B fail and
no engine parameters are available land the aircraft. Aircraft
Manufacturer is responsible for defining a procedure for both
failure conditions.
Loss of Power
Aircraft Manufacturer is responsible for defining a procedure for
this failure condition.
3.2) Failures during engine start
3.2.1) Engine does not start
Insufficient supply from electrical power source.
• Ensure that Engine starter and EMS system is supplied by an
external power source until engine reaches idle speed
Insufficient fuel supply.
• Ensure that Engine is supplied with fuel in appropriate quality
Starting at low oil temperature.
• Use high quality oil without friction modifier see Chapter 2.4).
3.3) Re-Start during flight
If the propeller continues to rotate during flight by windmilling,
but the speed is not sufficient to start the engine, the electric
starter can be used. It is not required to wait until the propeller
stops rotating.

BRP ROTAX 916 i A Series Specifications

General

Brand	BRP
Model	ROTAX 916 i A Series
Category	Engine
Language	English